Demonstrators for hybrid & innovative aeronautical propulsion systems


Developing the low-carbon aircraft of tomorrow is a key concern for all aviation industry players and of major concern for achieving sustainability in the aviation sector.

Hybrid Electric propulsion is identified as a promising technology to reduce emissions, covering a wide range of aircraft.

This project aims to:

  • Develop a predictive methodology for the dynamic calculation of hybrid shaft lines, validated on a partial bench,
  • Develop and test a hybrid electric turboprop ground demonstrator.